View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 21015U 90111B 25342.12896019 .00000402 00000-0 14335-3 0 9998
2 21015 74.0492 216.2925 0020394 73.7974 286.5422 14.37206541930351
| Epoch (UTC): | 08 December 2025 03:05:42 |
| Eccentricity: | 0.0020394 |
| inclination: | 74.0492° |
| perigee height: | 753 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 216.2925° |
| argument of perigee: | 73.7974° |
| revolutions per day: | 14.37206541 |
| mean anomaly at epoch: | 286.5422° |
| orbit number at epoch: | 93035 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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